Liquefaction of air in the Langley 11-inch hypersonic tunnel

Charles H. McLellan, Thomas W. Williamsnaca-tn-3302Oct 1954

Pressure and scattered-light measurements were made in the Langley 11-inch hypersonic tunnel to determine the effect of stagnation temperature on the flow in two Mach number 7 nozzles and to determine the nature of the condensation process occurring at low stagnation temperatures.